PZL M28 05
PZL Mielec
About
The third model on the PZL M28’s type certificate and the one certificated around what it carries rather than what it weighs: EASA.A.058 section C prints no maximum take-off or landing weight for it at all, giving instead a maximum zero-fuel weight of 6,900 kg, a maximum payload of 2,300 kg and a minimum weight for flight of 4,700 kg. A 700 kg hoist among its limitations says what the omission is about — this is the search-and-rescue M28. It shares the family airframe exactly: 13.10 m long, 22.06 m of wing span over 39.72 m², 4.90 m tall, two Pratt & Whitney Canada PT6A-65B turboprops, two pilots, and a maximum operating altitude of 7,620 m with crew oxygen or 3,000 m without. Seating depends on the fit: up to 19 passengers in pure passenger transport, 18 in a passenger-cargo mix and 13 in the improved standard.
Weightscompared to Airbus A318
Capacitycompared to Airbus A318
Passenger Capacity
14% of A318 maximum capacity
Crew
Dimensions
Length
Wingspan
Height
Wing Area
Sources11 figures on this page
- Type-Certificate Data Sheet No. EASA.A.058 for PZL M28EASA.A.058 rev Issue 12European Union Aviation Safety Agency · tier 1 · 11 figures · pages 23, 24, 25, 28
Engine Specifications
Engine Count
2×
Engine Model
Pratt & Whitney Canada PT6A-65B turboprop
Production & History
Production Status
In production
Business jets and the API are coming
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